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 00005U 26133.88342566 +.00000000 +00000-0 +14315-3 0 00002
2 00005 34.2487 60.1914 1836085 343.7946 11.0741 10.85981020 01
| Epoch (UTC): | 13 May 2026 21:12:07 |
| Eccentricity: | 0.1836085 |
| inclination: | 34.2487° |
| perigee height: | 654 km |
| apogee height: | 3817 km |
| right ascension of ascending node: | 60.1914° |
| argument of perigee: | 343.7946° |
| revolutions per day: | 10.85981020 |
| mean anomaly at epoch: | 11.0741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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