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 25320U 26088.19602525 +.00000000 +00000-0 +14098-3 0 00004
2 25320 86.3995 329.6223 0001420 153.7712 206.3559 14.41423791 00
| Epoch (UTC): | 29 March 2026 04:42:16 |
| Eccentricity: | 0.0001420 |
| inclination: | 86.3995° |
| perigee height: | 753 km |
| apogee height: | 755 km |
| right ascension of ascending node: | 329.6223° |
| argument of perigee: | 153.7712° |
| revolutions per day: | 14.41423791 |
| mean anomaly at epoch: | 206.3559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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