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 25979U 26159.49438534 +.00000000 +00000-0 +48152-3 0 00001
2 25979 98.1602 250.9582 0004880 128.1062 232.0619 15.34617789 05
| Epoch (UTC): | 08 June 2026 11:51:54 |
| Eccentricity: | 0.0004880 |
| inclination: | 98.1602° |
| perigee height: | 459 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 250.9582° |
| argument of perigee: | 128.1062° |
| revolutions per day: | 15.34617789 |
| mean anomaly at epoch: | 232.0619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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