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 25261U 26088.04350983 +.00000000 +00000-0 +16202-3 0 00009
2 25261 98.8234 117.1021 0003543 20.8861 339.2468 14.36287578 01
| Epoch (UTC): | 29 March 2026 01:02:39 |
| Eccentricity: | 0.0003543 |
| inclination: | 98.8234° |
| perigee height: | 768 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 117.1021° |
| argument of perigee: | 20.8861° |
| revolutions per day: | 14.36287578 |
| mean anomaly at epoch: | 339.2468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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