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 is defined by the following mean orbital elements,
1 37253U 26106.09539145 +.00000000 +00000-0 +31993-3 0 00002
2 37253 34.5262 50.4692 4010760 235.7049 79.7113 7.37277108 08
| Epoch (UTC): | 16 April 2026 02:17:21 |
| Eccentricity: | 0.4010760 |
| inclination: | 34.5262° |
| perigee height: | 300 km |
| apogee height: | 9245 km |
| right ascension of ascending node: | 50.4692° |
| argument of perigee: | 235.7049° |
| revolutions per day: | 7.37277108 |
| mean anomaly at epoch: | 79.7113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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