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 23151.43249189 .00005512 00000-0 31434-3 0 9998
2 12987 82.4995 280.9586 0019434 122.5849 237.7261 15.12414562260261
| Epoch (UTC): | 31 May 2023 10:22:47 |
| Eccentricity: | 0.0019434 |
| inclination: | 82.4995° |
| perigee height: | 515 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 280.9586° |
| argument of perigee: | 122.5849° |
| revolutions per day: | 15.12414562 |
| mean anomaly at epoch: | 237.7261° |
| orbit number at epoch: | 26026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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