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 25261U 26160.07431575 +.00000000 +00000-0 +11214-3 0 00008
2 25261 98.8146 190.8274 0004238 135.5075 224.6451 14.36341946 03
| Epoch (UTC): | 09 June 2026 01:47:00 |
| Eccentricity: | 0.0004238 |
| inclination: | 98.8146° |
| perigee height: | 768 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 190.8274° |
| argument of perigee: | 135.5075° |
| revolutions per day: | 14.36341946 |
| mean anomaly at epoch: | 224.6451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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