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 24920U 97047A 23334.12139306 .00000594 00000-0 26742-3 0 9996
2 24920 69.9535 313.2744 0019240 107.7613 252.5610 14.26936236366223
| Epoch (UTC): | 30 November 2023 02:54:48 |
| Eccentricity: | 0.0019240 |
| inclination: | 69.9535° |
| perigee height: | 788 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 313.2744° |
| argument of perigee: | 107.7613° |
| revolutions per day: | 14.26936236 |
| mean anomaly at epoch: | 252.5610° |
| orbit number at epoch: | 36622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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