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 25157U 26160.84690926 +.00000000 +00000-0 +70577-3 0 00001
2 25157 108.0039 142.9614 0023018 350.4044 9.6731 15.84496603 06
| Epoch (UTC): | 09 June 2026 20:19:32 |
| Eccentricity: | 0.0023018 |
| inclination: | 108.0039° |
| perigee height: | 302 km |
| apogee height: | 333 km |
| right ascension of ascending node: | 142.9614° |
| argument of perigee: | 350.4044° |
| revolutions per day: | 15.84496603 |
| mean anomaly at epoch: | 9.6731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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