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 48958U 21059CH 22222.51509461 .00002712 00000-0 14603-3 0 9991
2 48958 97.5627 352.4905 0015093 274.9156 85.0353 15.15607229 62169
| Epoch (UTC): | 10 August 2022 12:21:44 |
| Eccentricity: | 0.0015093 |
| inclination: | 97.5627° |
| perigee height: | 509 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 352.4905° |
| argument of perigee: | 274.9156° |
| revolutions per day: | 15.15607229 |
| mean anomaly at epoch: | 85.0353° |
| orbit number at epoch: | 6216 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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