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 46794U 26145.38275171 +.00000000 +00000-0 +12105-2 0 00006
2 46794 53.0401 283.8633 0005703 260.0247 100.0122 15.60649316 01
| Epoch (UTC): | 25 May 2026 09:11:09 |
| Eccentricity: | 0.0005703 |
| inclination: | 53.0401° |
| perigee height: | 382 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 283.8633° |
| argument of perigee: | 260.0247° |
| revolutions per day: | 15.60649316 |
| mean anomaly at epoch: | 100.0122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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