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 is defined by the following mean orbital elements,
1 12987U 26160.28027752 +.00000000 +00000-0 +24268-3 0 00003
2 12987 82.4899 257.2532 0010197 205.6113 154.4627 15.35634089 04
| Epoch (UTC): | 09 June 2026 06:43:35 |
| Eccentricity: | 0.0010197 |
| inclination: | 82.4899° |
| perigee height: | 452 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.2532° |
| argument of perigee: | 205.6113° |
| revolutions per day: | 15.35634089 |
| mean anomaly at epoch: | 154.4627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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