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 39010U 26068.76726498 +.00000000 +00000-0 +94811-3 0 00003
2 39010 49.6461 257.3963 4585662 60.6097 337.4486 6.31444667 00
| Epoch (UTC): | 09 March 2026 18:24:51 |
| Eccentricity: | 0.4585662 |
| inclination: | 49.6461° |
| perigee height: | 316 km |
| apogee height: | 11656 km |
| right ascension of ascending node: | 257.3963° |
| argument of perigee: | 60.6097° |
| revolutions per day: | 6.31444667 |
| mean anomaly at epoch: | 337.4486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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