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 25980U 26087.98402272 +.00000000 +00000-0 +33539-3 0 00000
2 25980 45.0308 180.9224 0005396 340.5015 19.5627 14.38021602 00
| Epoch (UTC): | 28 March 2026 23:36:59 |
| Eccentricity: | 0.0005396 |
| inclination: | 45.0308° |
| perigee height: | 761 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 180.9224° |
| argument of perigee: | 340.5015° |
| revolutions per day: | 14.38021602 |
| mean anomaly at epoch: | 19.5627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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