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 25736U 26150.55129506 +.00000000 +00000-0 +31985-3 0 00002
2 25736 97.6871 11.7465 0003244 303.1188 56.9701 14.57164436 03
| Epoch (UTC): | 30 May 2026 13:13:51 |
| Eccentricity: | 0.0003244 |
| inclination: | 97.6871° |
| perigee height: | 700 km |
| apogee height: | 705 km |
| right ascension of ascending node: | 11.7465° |
| argument of perigee: | 303.1188° |
| revolutions per day: | 14.57164436 |
| mean anomaly at epoch: | 56.9701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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