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 22276U 26070.82170670 +.00000000 +00000-0 +28898-3 0 00006
2 22276 20.2845 255.1968 0050070 212.0246 147.7132 14.95858221 07
| Epoch (UTC): | 11 March 2026 19:43:15 |
| Eccentricity: | 0.0050070 |
| inclination: | 20.2845° |
| perigee height: | 545 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 255.1968° |
| argument of perigee: | 212.0246° |
| revolutions per day: | 14.95858221 |
| mean anomaly at epoch: | 147.7132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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