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 26068.53624100 +.00000000 +00000-0 +10794-3 0 00000
2 25940 98.8521 75.2771 0003960 298.3954 61.6832 14.36960536 01
| Epoch (UTC): | 09 March 2026 12:52:11 |
| Eccentricity: | 0.0003960 |
| inclination: | 98.8521° |
| perigee height: | 766 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 75.2771° |
| argument of perigee: | 298.3954° |
| revolutions per day: | 14.36960536 |
| mean anomaly at epoch: | 61.6832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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