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 22237U 92080B 25082.82297188 .00001378 00000-0 17909-3 0 9995
2 22237 82.5152 357.6077 0017673 286.6575 73.2697 14.79949356742531
| Epoch (UTC): | 23 March 2025 19:45:04 |
| Eccentricity: | 0.0017673 |
| inclination: | 82.5152° |
| perigee height: | 617 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 357.6077° |
| argument of perigee: | 286.6575° |
| revolutions per day: | 14.79949356 |
| mean anomaly at epoch: | 73.2697° |
| orbit number at epoch: | 74253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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