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 25159U 26150.83644205 +.00000000 +00000-0 +47008-3 0 00003
2 25159 107.9624 133.7103 0040723 354.7480 5.3229 14.35704310 07
| Epoch (UTC): | 30 May 2026 20:04:28 |
| Eccentricity: | 0.0040723 |
| inclination: | 107.9624° |
| perigee height: | 744 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 133.7103° |
| argument of perigee: | 354.7480° |
| revolutions per day: | 14.35704310 |
| mean anomaly at epoch: | 5.3229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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