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 39253U 26145.51847918 +.00000000 +00000-0 +10124-3 0 00007
2 39253 29.7218 335.2589 0136795 193.1843 166.5131 13.55541699 09
| Epoch (UTC): | 25 May 2026 12:26:36 |
| Eccentricity: | 0.0136795 |
| inclination: | 29.7218° |
| perigee height: | 950 km |
| apogee height: | 1154 km |
| right ascension of ascending node: | 335.2589° |
| argument of perigee: | 193.1843° |
| revolutions per day: | 13.55541699 |
| mean anomaly at epoch: | 166.5131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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