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 26106.53732411 +.00000000 +00000-0 +12260-3 0 00003
2 26061 100.2235 99.2422 0032386 47.0630 313.3264 14.45036320 00
| Epoch (UTC): | 16 April 2026 12:53:44 |
| Eccentricity: | 0.0032386 |
| inclination: | 100.2235° |
| perigee height: | 719 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 99.2422° |
| argument of perigee: | 47.0630° |
| revolutions per day: | 14.45036320 |
| mean anomaly at epoch: | 313.3264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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