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 26061U 26087.91151837 +.00000000 +00000-0 +23073-3 0 00004
2 26061 100.2225 76.8586 0032513 98.9596 261.5272 14.45006880 00
| Epoch (UTC): | 28 March 2026 21:52:35 |
| Eccentricity: | 0.0032513 |
| inclination: | 100.2225° |
| perigee height: | 719 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 76.8586° |
| argument of perigee: | 98.9596° |
| revolutions per day: | 14.45006880 |
| mean anomaly at epoch: | 261.5272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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