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 36827U 10028F 23083.55466407 .00001232 00000-0 37770-3 0 9995
2 36827 98.5320 281.4777 0042271 189.8358 170.2009 14.42950740532510
| Epoch (UTC): | 24 March 2023 13:18:42 |
| Eccentricity: | 0.0042271 |
| inclination: | 98.5320° |
| perigee height: | 718 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 281.4777° |
| argument of perigee: | 189.8358° |
| revolutions per day: | 14.42950740 |
| mean anomaly at epoch: | 170.2009° |
| orbit number at epoch: | 53251 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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