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 40968U 26032.04463689 +.00000000 +00000-0 +34927-3 0 00001
2 40968 64.7775 324.8589 0119121 108.0562 253.3572 14.94626187 06
| Epoch (UTC): | 01 February 2026 01:04:16 |
| Eccentricity: | 0.0119121 |
| inclination: | 64.7775° |
| perigee height: | 501 km |
| apogee height: | 666 km |
| right ascension of ascending node: | 324.8589° |
| argument of perigee: | 108.0562° |
| revolutions per day: | 14.94626187 |
| mean anomaly at epoch: | 253.3572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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