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 25876U 26021.50521205 +.00000000 +00000-0 +70201-3 0 00005
2 25876 51.7630 129.6928 0503224 209.0199 148.1881 14.11594664 07
| Epoch (UTC): | 21 January 2026 12:07:30 |
| Eccentricity: | 0.0503224 |
| inclination: | 51.7630° |
| perigee height: | 490 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 129.6928° |
| argument of perigee: | 209.0199° |
| revolutions per day: | 14.11594664 |
| mean anomaly at epoch: | 148.1881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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