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 56914U 26145.00155493 +.00000000 +00000-0 +39334-4 0 00009
2 56914 43.0045 359.3132 0001282 255.3164 104.7546 15.27574663 01
| Epoch (UTC): | 25 May 2026 00:02:14 |
| Eccentricity: | 0.0001282 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 359.3132° |
| argument of perigee: | 255.3164° |
| revolutions per day: | 15.27574663 |
| mean anomaly at epoch: | 104.7546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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