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 22676U 26067.57449438 +.00000000 +00000-0 +83958-4 0 00008
2 22676 74.0403 110.9908 0016946 76.9750 283.3293 14.35262597 05
| Epoch (UTC): | 08 March 2026 13:47:16 |
| Eccentricity: | 0.0016946 |
| inclination: | 74.0403° |
| perigee height: | 762 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 110.9908° |
| argument of perigee: | 76.9750° |
| revolutions per day: | 14.35262597 |
| mean anomaly at epoch: | 283.3293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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