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 23336.84946394 .00000175 00000-0 11877-3 0 9998
2 00059 28.2463 208.1726 0189053 90.6662 271.5548 13.53050099117479
| Epoch (UTC): | 02 December 2023 20:23:13 |
| Eccentricity: | 0.0189053 |
| inclination: | 28.2463° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 208.1726° |
| argument of perigee: | 90.6662° |
| revolutions per day: | 13.53050099 |
| mean anomaly at epoch: | 271.5548° |
| orbit number at epoch: | 11747 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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