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 26042.06479757 +.00000000 +00000-0 +16292-3 0 00001
2 25261 98.8294 70.0080 0004296 128.5199 231.6372 14.36243231 02
| Epoch (UTC): | 11 February 2026 01:33:18 |
| Eccentricity: | 0.0004296 |
| inclination: | 98.8294° |
| perigee height: | 768 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 70.0080° |
| argument of perigee: | 128.5199° |
| revolutions per day: | 14.36243231 |
| mean anomaly at epoch: | 231.6372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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