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 26931U 26038.87297574 +.00000000 +00000-0 +11296-3 0 00004
2 26931 67.0487 218.7237 0007046 266.3665 93.6631 14.31894613 04
| Epoch (UTC): | 07 February 2026 20:57:05 |
| Eccentricity: | 0.0007046 |
| inclination: | 67.0487° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 218.7237° |
| argument of perigee: | 266.3665° |
| revolutions per day: | 14.31894613 |
| mean anomaly at epoch: | 93.6631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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