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 23851U 96024A 25118.45394775 .00000061 00000-0 73387-4 0 9990
2 23851 99.0046 57.3676 0006580 303.6933 56.3603 13.98332400480355
| Epoch (UTC): | 28 April 2025 10:53:41 |
| Eccentricity: | 0.0006580 |
| inclination: | 99.0046° |
| perigee height: | 895 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 57.3676° |
| argument of perigee: | 303.6933° |
| revolutions per day: | 13.98332400 |
| mean anomaly at epoch: | 56.3603° |
| orbit number at epoch: | 48035 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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