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 25757U 26088.24225216 +.00000000 +00000-0 +51211-4 0 00001
2 25757 98.6681 81.1257 0013274 230.4491 129.5531 14.52404644 00
| Epoch (UTC): | 29 March 2026 05:48:50 |
| Eccentricity: | 0.0013274 |
| inclination: | 98.6681° |
| perigee height: | 708 km |
| apogee height: | 727 km |
| right ascension of ascending node: | 81.1257° |
| argument of perigee: | 230.4491° |
| revolutions per day: | 14.52404644 |
| mean anomaly at epoch: | 129.5531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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