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 28895U 05043F 24340.33007947 .00005315 00000-0 90204-3 0 9992
2 28895 98.2239 116.8603 0015229 173.3704 186.7705 14.69550803 19573
| Epoch (UTC): | 05 December 2024 07:55:18 |
| Eccentricity: | 0.0015229 |
| inclination: | 98.2239° |
| perigee height: | 652 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 116.8603° |
| argument of perigee: | 173.3704° |
| revolutions per day: | 14.69550803 |
| mean anomaly at epoch: | 186.7705° |
| orbit number at epoch: | 1957 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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