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 25725U 26044.51799330 +.00000000 +00000-0 +28024-3 0 00006
2 25725 28.3320 76.6673 2384004 294.1352 42.8644 9.67465744 03
| Epoch (UTC): | 13 February 2026 12:25:54 |
| Eccentricity: | 0.2384004 |
| inclination: | 28.3320° |
| perigee height: | 707 km |
| apogee height: | 5143 km |
| right ascension of ascending node: | 76.6673° |
| argument of perigee: | 294.1352° |
| revolutions per day: | 9.67465744 |
| mean anomaly at epoch: | 42.8644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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