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 00011U 26083.98974525 +.00000000 +00000-0 +51588-3 0 00003
2 00011 32.8772 43.7815 1445518 297.7180 48.4153 11.90294995 07
| Epoch (UTC): | 24 March 2026 23:45:13 |
| Eccentricity: | 0.1445518 |
| inclination: | 32.8772° |
| perigee height: | 553 km |
| apogee height: | 2896 km |
| right ascension of ascending node: | 43.7815° |
| argument of perigee: | 297.7180° |
| revolutions per day: | 11.90294995 |
| mean anomaly at epoch: | 48.4153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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