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 21667U 26065.40139307 +.00000000 +00000-0 +91003-4 0 00008
2 21667 82.9097 157.6732 0020937 21.0293 49.8520 13.75280720 01
| Epoch (UTC): | 06 March 2026 09:38:00 |
| Eccentricity: | 0.0020937 |
| inclination: | 82.9097° |
| perigee height: | 965 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 157.6732° |
| argument of perigee: | 21.0293° |
| revolutions per day: | 13.75280720 |
| mean anomaly at epoch: | 49.8520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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