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 20625U 90046B 24280.80038483 .00000035 00000-0 42678-4 0 9993
2 20625 70.9994 307.5757 0014078 2.6119 357.5074 14.14884167774999
| Epoch (UTC): | 06 October 2024 19:12:33 |
| Eccentricity: | 0.0014078 |
| inclination: | 70.9994° |
| perigee height: | 832 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 307.5757° |
| argument of perigee: | 2.6119° |
| revolutions per day: | 14.14884167 |
| mean anomaly at epoch: | 357.5074° |
| orbit number at epoch: | 77499 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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