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 26100.23644683 +.00000000 +00000-0 +21234-3 0 00008
2 26061 100.2233 91.6694 0032508 64.6392 295.8153 14.45030953 08
| Epoch (UTC): | 10 April 2026 05:40:29 |
| Eccentricity: | 0.0032508 |
| inclination: | 100.2233° |
| perigee height: | 719 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 91.6694° |
| argument of perigee: | 64.6392° |
| revolutions per day: | 14.45030953 |
| mean anomaly at epoch: | 295.8153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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