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 26017.68151727 +.00000000 +00000-0 +14120-3 0 00003
2 25261 98.8310 45.0280 0003154 193.2604 166.8499 14.36211300 08
| Epoch (UTC): | 17 January 2026 16:21:23 |
| Eccentricity: | 0.0003154 |
| inclination: | 98.8310° |
| perigee height: | 769 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 45.0280° |
| argument of perigee: | 193.2604° |
| revolutions per day: | 14.36211300 |
| mean anomaly at epoch: | 166.8499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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