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 26103.61910500 +.00000000 +00000-0 +42114-3 0 00009
2 26621 95.4077 58.9227 0711940 58.4585 308.4072 13.04826930 01
| Epoch (UTC): | 13 April 2026 14:51:30 |
| Eccentricity: | 0.0711940 |
| inclination: | 95.4077° |
| perigee height: | 701 km |
| apogee height: | 1786 km |
| right ascension of ascending node: | 58.9227° |
| argument of perigee: | 58.4585° |
| revolutions per day: | 13.04826930 |
| mean anomaly at epoch: | 308.4072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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