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 05118U 71028B 25189.55101699 .00013071 00000-0 26532-3 0 9997
2 05118 81.2420 349.5045 0024631 71.3876 289.0040 15.45870523950795
| Epoch (UTC): | 08 July 2025 13:13:27 |
| Eccentricity: | 0.0024631 |
| inclination: | 81.2420° |
| perigee height: | 412 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 349.5045° |
| argument of perigee: | 71.3876° |
| revolutions per day: | 15.45870523 |
| mean anomaly at epoch: | 289.0040° |
| orbit number at epoch: | 95079 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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