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 05917U 72022A 23156.82139156 .00000251 00000-0 13773-3 0 9999
2 05917 81.2214 283.6958 0030152 214.6275 145.2933 14.08834520628492
| Epoch (UTC): | 05 June 2023 19:42:48 |
| Eccentricity: | 0.0030152 |
| inclination: | 81.2214° |
| perigee height: | 841 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 283.6958° |
| argument of perigee: | 214.6275° |
| revolutions per day: | 14.08834520 |
| mean anomaly at epoch: | 145.2933° |
| orbit number at epoch: | 62849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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