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 40039U 26156.39498808 +.00000000 +00000-0 +24318-3 0 00009
2 40039 97.9642 100.3340 0010951 345.5802 14.5104 14.95594170 09
| Epoch (UTC): | 05 June 2026 09:28:46 |
| Eccentricity: | 0.0010951 |
| inclination: | 97.9642° |
| perigee height: | 573 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 100.3340° |
| argument of perigee: | 345.5802° |
| revolutions per day: | 14.95594170 |
| mean anomaly at epoch: | 14.5104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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