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 25983U 26100.01163610 +.00000000 +00000-0 +31504-3 0 00003
2 25983 45.0300 26.8099 0007080 109.8969 250.2644 14.40863615 03
| Epoch (UTC): | 10 April 2026 00:16:45 |
| Eccentricity: | 0.0007080 |
| inclination: | 45.0300° |
| perigee height: | 751 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 26.8099° |
| argument of perigee: | 109.8969° |
| revolutions per day: | 14.40863615 |
| mean anomaly at epoch: | 250.2644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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