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 25501U 98058A 21015.54506094 -.00000035 00000-0 00000-0 0 9994
2 25501 9.2022 28.9093 0015248 316.0574 55.1804 0.98175239 80406
| Epoch (UTC): | 15 January 2021 13:04:53 |
| Eccentricity: | 0.0015248 |
| inclination: | 9.2022° |
| perigee height: | 36319 km |
| apogee height: | 36449 km |
| right ascension of ascending node: | 28.9093° |
| argument of perigee: | 316.0574° |
| revolutions per day: | 0.98175239 |
| mean anomaly at epoch: | 55.1804° |
| orbit number at epoch: | 8040 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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