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 41337U 26150.39036355 +.00000000 +00000-0 +16463-3 0 00002
2 41337 30.9978 189.1204 0009461 74.2334 285.9347 15.10429984 05
| Epoch (UTC): | 30 May 2026 09:22:07 |
| Eccentricity: | 0.0009461 |
| inclination: | 30.9978° |
| perigee height: | 528 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 189.1204° |
| argument of perigee: | 74.2334° |
| revolutions per day: | 15.10429984 |
| mean anomaly at epoch: | 285.9347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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