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 12987U 81117A 23152.62339101 .00006134 00000-0 34987-3 0 9991
2 12987 82.4999 279.7883 0019396 118.9049 241.4131 15.12429689260140
| Epoch (UTC): | 01 June 2023 14:57:40 |
| Eccentricity: | 0.0019396 |
| inclination: | 82.4999° |
| perigee height: | 515 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 279.7883° |
| argument of perigee: | 118.9049° |
| revolutions per day: | 15.12429689 |
| mean anomaly at epoch: | 241.4131° |
| orbit number at epoch: | 26014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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