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 25401U 26088.11675762 +.00000000 +00000-0 +24169-3 0 00009
2 25401 98.5371 217.0251 0160712 198.7053 345.9733 13.94813199 07
| Epoch (UTC): | 29 March 2026 02:48:07 |
| Eccentricity: | 0.0160712 |
| inclination: | 98.5371° |
| perigee height: | 795 km |
| apogee height: | 1029 km |
| right ascension of ascending node: | 217.0251° |
| argument of perigee: | 198.7053° |
| revolutions per day: | 13.94813199 |
| mean anomaly at epoch: | 345.9733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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