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 39640U 26155.29409050 +.00000000 +00000-0 +14249-3 0 00006
2 39640 65.0103 39.9016 0018044 281.5673 78.3387 14.34252599 06
| Epoch (UTC): | 04 June 2026 07:03:29 |
| Eccentricity: | 0.0018044 |
| inclination: | 65.0103° |
| perigee height: | 765 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 39.9016° |
| argument of perigee: | 281.5673° |
| revolutions per day: | 14.34252599 |
| mean anomaly at epoch: | 78.3387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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