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 26621U 26150.77492890 +.00000000 +00000-0 -31534-3 0 00000
2 26621 95.4123 82.8817 0709027 296.9497 56.0905 13.04837228 01
| Epoch (UTC): | 30 May 2026 18:35:53 |
| Eccentricity: | 0.0709027 |
| inclination: | 95.4123° |
| perigee height: | 703 km |
| apogee height: | 1784 km |
| right ascension of ascending node: | 82.8817° |
| argument of perigee: | 296.9497° |
| revolutions per day: | 13.04837228 |
| mean anomaly at epoch: | 56.0905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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