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 26018.47102222 +.00000000 +00000-0 +73496-4 0 00003
2 25940 98.8495 23.8064 0005990 81.7271 278.4593 14.36926092 07
| Epoch (UTC): | 18 January 2026 11:18:16 |
| Eccentricity: | 0.0005990 |
| inclination: | 98.8495° |
| perigee height: | 764 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 23.8064° |
| argument of perigee: | 81.7271° |
| revolutions per day: | 14.36926092 |
| mean anomaly at epoch: | 278.4593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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