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 26151.08587617 +.00000000 +00000-0 +72206-3 0 00000
2 37253 34.5157 336.1574 4009430 343.6173 6.4881 7.37695763 03
| Epoch (UTC): | 31 May 2026 02:03:39 |
| Eccentricity: | 0.4009430 |
| inclination: | 34.5157° |
| perigee height: | 299 km |
| apogee height: | 9238 km |
| right ascension of ascending node: | 336.1574° |
| argument of perigee: | 343.6173° |
| revolutions per day: | 7.37695763 |
| mean anomaly at epoch: | 6.4881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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