View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 4659U 70025AT 24358.15552280 .00003467 00000-0 27792-2 0 9997
2 4659 100.0963 62.3787 0012811 242.6282 117.3571 13.91452042733826
| Epoch (UTC): | 23 December 2024 03:43:57 |
| Eccentricity: | 0.0012811 |
| inclination: | 100.0963° |
| perigee height: | 914 km |
| apogee height: | 933 km |
| right ascension of ascending node: | 62.3787° |
| argument of perigee: | 242.6282° |
| revolutions per day: | 13.91452042 |
| mean anomaly at epoch: | 117.3571° |
| orbit number at epoch: | 73382 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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