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 26088.17084884 +.00000000 +00000-0 +36360-3 0 00005
2 40968 64.7753 149.3624 0116847 85.1490 276.2954 14.95235015 04
| Epoch (UTC): | 29 March 2026 04:06:01 |
| Eccentricity: | 0.0116847 |
| inclination: | 64.7753° |
| perigee height: | 500 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 149.3624° |
| argument of perigee: | 85.1490° |
| revolutions per day: | 14.95235015 |
| mean anomaly at epoch: | 276.2954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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