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 26142.39063413 +.00000000 +00000-0 +21335-4 0 00001
2 25757 98.6693 137.0471 0015336 70.3929 289.8920 14.52418902 04
| Epoch (UTC): | 22 May 2026 09:22:30 |
| Eccentricity: | 0.0015336 |
| inclination: | 98.6693° |
| perigee height: | 707 km |
| apogee height: | 729 km |
| right ascension of ascending node: | 137.0471° |
| argument of perigee: | 70.3929° |
| revolutions per day: | 14.52418902 |
| mean anomaly at epoch: | 289.8920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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