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 25135U 26037.25476897 +.00000000 +00000-0 +47929-4 0 00000
2 25135 26.8856 358.3670 0355259 140.3725 355.0942 13.62761868 02
| Epoch (UTC): | 06 February 2026 06:06:52 |
| Eccentricity: | 0.0355259 |
| inclination: | 26.8856° |
| perigee height: | 763 km |
| apogee height: | 1289 km |
| right ascension of ascending node: | 358.3670° |
| argument of perigee: | 140.3725° |
| revolutions per day: | 13.62761868 |
| mean anomaly at epoch: | 355.0942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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