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 39765U 26141.29556005 +.00000000 +00000-0 +15948-4 0 00000
2 39765 82.4485 270.5732 0232397 64.9496 297.5537 12.82902528 00
| Epoch (UTC): | 21 May 2026 07:05:36 |
| Eccentricity: | 0.0232397 |
| inclination: | 82.4485° |
| perigee height: | 1151 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 270.5732° |
| argument of perigee: | 64.9496° |
| revolutions per day: | 12.82902528 |
| mean anomaly at epoch: | 297.5537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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