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 06797U 26040.05243951 +.00000000 +00000-0 +85168-3 0 00004
2 06797 27.2262 229.3105 7236297 221.2399 52.1611 2.21915978 08
| Epoch (UTC): | 09 February 2026 01:15:30 |
| Eccentricity: | 0.7236297 |
| inclination: | 27.2262° |
| perigee height: | 484 km |
| apogee height: | 36416 km |
| right ascension of ascending node: | 229.3105° |
| argument of perigee: | 221.2399° |
| revolutions per day: | 2.21915978 |
| mean anomaly at epoch: | 52.1611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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