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 41891U 26145.07620523 +.00000000 +00000-0 +31709-3 0 00002
2 41891 34.9417 25.2164 0007836 316.9957 43.0154 15.58745490 02
| Epoch (UTC): | 25 May 2026 01:49:44 |
| Eccentricity: | 0.0007836 |
| inclination: | 34.9417° |
| perigee height: | 386 km |
| apogee height: | 397 km |
| right ascension of ascending node: | 25.2164° |
| argument of perigee: | 316.9957° |
| revolutions per day: | 15.58745490 |
| mean anomaly at epoch: | 43.0154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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