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 22279.82088649 .00000129 00000-0 52911-4 0 9995
2 00059 28.2473 216.2137 0189285 148.1289 213.0863 13.53007047 60278
| Epoch (UTC): | 06 October 2022 19:42:04 |
| Eccentricity: | 0.0189285 |
| inclination: | 28.2473° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 216.2137° |
| argument of perigee: | 148.1289° |
| revolutions per day: | 13.53007047 |
| mean anomaly at epoch: | 213.0863° |
| orbit number at epoch: | 6027 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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