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 21231U 26038.19988853 +.00000000 +00000-0 +69892-4 0 00000
2 21231 82.9518 289.6333 0036355 49.4276 61.7312 13.76109456 04
| Epoch (UTC): | 07 February 2026 04:47:50 |
| Eccentricity: | 0.0036355 |
| inclination: | 82.9518° |
| perigee height: | 951 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 289.6333° |
| argument of perigee: | 49.4276° |
| revolutions per day: | 13.76109456 |
| mean anomaly at epoch: | 61.7312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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