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 00005U 26073.55236720 +.00000000 +00000-0 +22484-3 0 00009
2 00005 34.2418 246.3722 1837205 71.7661 307.3546 10.85958397 02
| Epoch (UTC): | 14 March 2026 13:15:24 |
| Eccentricity: | 0.1837205 |
| inclination: | 34.2418° |
| perigee height: | 653 km |
| apogee height: | 3818 km |
| right ascension of ascending node: | 246.3722° |
| argument of perigee: | 71.7661° |
| revolutions per day: | 10.85958397 |
| mean anomaly at epoch: | 307.3546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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