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 00059U 60013B 23080.24014543 .00000139 00000-0 70146-4 0 9995
2 00059 28.2476 86.4388 0189290 96.6322 265.5805 13.53023987 82696
| Epoch (UTC): | 21 March 2023 05:45:48 |
| Eccentricity: | 0.0189290 |
| inclination: | 28.2476° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 86.4388° |
| argument of perigee: | 96.6322° |
| revolutions per day: | 13.53023987 |
| mean anomaly at epoch: | 265.5805° |
| orbit number at epoch: | 8269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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