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 00082U 61004B 22176.48487599 -.00000023 00000-0 32270-4 0 9997
2 00082 38.8564 345.6725 1171638 45.2406 323.7820 12.26016320898391
| Epoch (UTC): | 25 June 2022 11:38:13 |
| Eccentricity: | 0.1171638 |
| inclination: | 38.8564° |
| perigee height: | 635 km |
| apogee height: | 2497 km |
| right ascension of ascending node: | 345.6725° |
| argument of perigee: | 45.2406° |
| revolutions per day: | 12.26016320 |
| mean anomaly at epoch: | 323.7820° |
| orbit number at epoch: | 89839 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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