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 26159.23356782 +.00000000 +00000-0 +46064-3 0 00007
2 25979 98.1602 250.6698 0004867 128.7404 231.4272 15.34609150 02
| Epoch (UTC): | 08 June 2026 05:36:20 |
| Eccentricity: | 0.0004867 |
| inclination: | 98.1602° |
| perigee height: | 459 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 250.6698° |
| argument of perigee: | 128.7404° |
| revolutions per day: | 15.34609150 |
| mean anomaly at epoch: | 231.4272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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