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 22568U 26088.08802484 +.00000000 +00000-0 +38057-3 0 00000
2 22568 75.7466 208.5239 0146269 332.6546 208.4439 14.45144050 04
| Epoch (UTC): | 29 March 2026 02:06:45 |
| Eccentricity: | 0.0146269 |
| inclination: | 75.7466° |
| perigee height: | 637 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 208.5239° |
| argument of perigee: | 332.6546° |
| revolutions per day: | 14.45144050 |
| mean anomaly at epoch: | 208.4439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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