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 26144.94568785 +.00000000 +00000-0 +32690-3 0 00002
2 40968 64.7761 331.6861 0117942 62.4072 298.8962 14.95704581 01
| Epoch (UTC): | 24 May 2026 22:41:47 |
| Eccentricity: | 0.0117942 |
| inclination: | 64.7761° |
| perigee height: | 498 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 331.6861° |
| argument of perigee: | 62.4072° |
| revolutions per day: | 14.95704581 |
| mean anomaly at epoch: | 298.8962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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