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  2. Mean anomaly - Wikipedia

    en.wikipedia.org/wiki/Mean_anomaly

    The mean anomaly at epoch, M 0, is defined as the instantaneous mean anomaly at a given epoch, t 0. This value is sometimes provided with other orbital elements to enable calculations of the object's past and future positions along the orbit. The epoch for which M 0 is defined is

  3. Epoch (astronomy) - Wikipedia

    en.wikipedia.org/wiki/Epoch_(astronomy)

    where the epoch is expressed in terms of Terrestrial Time, with an equivalent Julian date. Four of the elements are independent of any particular coordinate system: M is mean anomaly (deg), n: mean daily motion (deg/d), a: size of semi-major axis (AU), e: eccentricity (dimensionless).

  4. Mean motion - Wikipedia

    en.wikipedia.org/wiki/Mean_motion

    where M 1 and M 0 are the mean anomalies at particular points in time, and Δt (≡ t 1-t 0) is the time elapsed between the two. M 0 is referred to as the mean anomaly at epoch t 0, and Δt is the time since epoch.

  5. Orbital elements - Wikipedia

    en.wikipedia.org/wiki/Orbital_elements

    Either the longitude at epoch, L 0, the mean anomaly at epoch, M 0, or the time of perihelion passage, T 0, are used to specify a known point in the orbit. The choices made depend whether the vernal equinox or the node are used as the primary reference. The semi-major axis is known if the mean motion and the gravitational mass are known. [2] [3]

  6. Mean longitude - Wikipedia

    en.wikipedia.org/wiki/Mean_longitude

    Then mean longitude is also [1] L = ϖ + M. Another form often seen is the mean longitude at epoch, ε. This is simply the mean longitude at a reference time t 0, known as the epoch. Mean longitude can then be expressed, [2] L = ε + n(t − t 0), or L = ε + nt, since t = 0 at the epoch t 0. where n is the mean angular motion and t is any ...

  7. List of common astronomy symbols - Wikipedia

    en.wikipedia.org/wiki/List_of_common_astronomy...

    M - Mean anomaly; M o - Mean anomaly at epoch; Radius comparison. Radius comparison: R E, R ...

  8. Two-line element set - Wikipedia

    en.wikipedia.org/wiki/Two-line_element_set

    A two-line element set (TLE, or more rarely 2LE) or three-line element set (3LE) is a data format encoding a list of orbital elements of an Earth-orbiting object for a given point in time, the epoch. Using a suitable prediction formula, the state (position and velocity) at any point in the past or future can be estimated to some accuracy.

  9. (532037) 2013 FY27 - Wikipedia

    en.wikipedia.org/wiki/(532037)_2013_FY27

    Epoch 2023 Feb 25 (JD 2460000.5) Uncertainty parameter 4: Observation arc: 3953 days (10.82 yr) Earliest precovery date: 15 March 2011 : ... Mean anomaly. 215.947 ...