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 26161.60666507 +.00000000 +00000-0 +23607-3 0 00009
2 25736 97.6861 21.9522 0002998 251.6137 108.4738 14.57192902 07
| Epoch (UTC): | 10 June 2026 14:33:35 |
| Eccentricity: | 0.0002998 |
| inclination: | 97.6861° |
| perigee height: | 700 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 21.9522° |
| argument of perigee: | 251.6137° |
| revolutions per day: | 14.57192902 |
| mean anomaly at epoch: | 108.4738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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