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 08294U 26040.50647609 +.00000000 +00000-0 +12056-3 0 00002
2 08294 81.2101 182.4745 0103562 124.8692 236.2269 14.09081103 05
| Epoch (UTC): | 09 February 2026 12:09:19 |
| Eccentricity: | 0.0103562 |
| inclination: | 81.2101° |
| perigee height: | 788 km |
| apogee height: | 938 km |
| right ascension of ascending node: | 182.4745° |
| argument of perigee: | 124.8692° |
| revolutions per day: | 14.09081103 |
| mean anomaly at epoch: | 236.2269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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