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 25140.56145767 .00000443 00000-0 55314-4 0 9991
2 22237 82.5095 303.7453 0020666 95.4321 264.9250 14.80029098751075
| Epoch (UTC): | 20 May 2025 13:28:29 |
| Eccentricity: | 0.0020666 |
| inclination: | 82.5095° |
| perigee height: | 615 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 303.7453° |
| argument of perigee: | 95.4321° |
| revolutions per day: | 14.80029098 |
| mean anomaly at epoch: | 264.9250° |
| orbit number at epoch: | 75107 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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