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 25940U 26070.55553933 +.00000000 +00000-0 +10280-3 0 00000
2 25940 98.8520 77.3536 0003883 290.7884 69.2885 14.36961819 01
| Epoch (UTC): | 11 March 2026 13:19:58 |
| Eccentricity: | 0.0003883 |
| inclination: | 98.8520° |
| perigee height: | 766 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 77.3536° |
| argument of perigee: | 290.7884° |
| revolutions per day: | 14.36961819 |
| mean anomaly at epoch: | 69.2885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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