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 23150.44006725 .00005426 00000-0 30955-3 0 9996
2 12987 82.4992 281.9338 0019434 125.6143 234.6902 15.12403327259819
| Epoch (UTC): | 30 May 2023 10:33:41 |
| Eccentricity: | 0.0019434 |
| inclination: | 82.4992° |
| perigee height: | 515 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 281.9338° |
| argument of perigee: | 125.6143° |
| revolutions per day: | 15.12403327 |
| mean anomaly at epoch: | 234.6902° |
| orbit number at epoch: | 25981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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