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 56701U 26145.47805576 +.00000000 +00000-0 +43718-4 0 00009
2 56701 43.0023 197.4219 0001761 260.2789 99.7864 15.27566443 01
| Epoch (UTC): | 25 May 2026 11:28:24 |
| Eccentricity: | 0.0001761 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.4219° |
| argument of perigee: | 260.2789° |
| revolutions per day: | 15.27566443 |
| mean anomaly at epoch: | 99.7864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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