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 28811U 05031C 25342.98909492 -.00000237 00000-0 -62633-4 0 9993
2 28811 97.7719 20.2625 0409790 188.2599 171.1683 14.00839542 36967
| Epoch (UTC): | 08 December 2025 23:44:17 |
| Eccentricity: | 0.0409790 |
| inclination: | 97.7719° |
| perigee height: | 593 km |
| apogee height: | 1189 km |
| right ascension of ascending node: | 20.2625° |
| argument of perigee: | 188.2599° |
| revolutions per day: | 14.00839542 |
| mean anomaly at epoch: | 171.1683° |
| orbit number at epoch: | 3696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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