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 22827U 93061E 24358.17847017 .00000460 00000-0 18739-3 0 9998
2 22827 98.7145 55.3160 0009006 172.8430 251.9026 14.32181403630873
| Epoch (UTC): | 23 December 2024 04:16:59 |
| Eccentricity: | 0.0009006 |
| inclination: | 98.7145° |
| perigee height: | 778 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 55.3160° |
| argument of perigee: | 172.8430° |
| revolutions per day: | 14.32181403 |
| mean anomaly at epoch: | 251.9026° |
| orbit number at epoch: | 63087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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