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 26032.50874912 +.00000000 +00000-0 +47300-4 0 00006
2 25757 98.6617 23.6039 0015046 46.0368 314.2064 14.52381652 08
| Epoch (UTC): | 01 February 2026 12:12:35 |
| Eccentricity: | 0.0015046 |
| inclination: | 98.6617° |
| perigee height: | 707 km |
| apogee height: | 729 km |
| right ascension of ascending node: | 23.6039° |
| argument of perigee: | 46.0368° |
| revolutions per day: | 14.52381652 |
| mean anomaly at epoch: | 314.2064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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