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 25981U 26087.97121977 +.00000000 +00000-0 +29752-3 0 00002
2 25981 45.0221 174.4221 0002385 358.8628 1.2214 14.37941486 07
| Epoch (UTC): | 28 March 2026 23:18:33 |
| Eccentricity: | 0.0002385 |
| inclination: | 45.0221° |
| perigee height: | 764 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 174.4221° |
| argument of perigee: | 358.8628° |
| revolutions per day: | 14.37941486 |
| mean anomaly at epoch: | 1.2214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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