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 39152U 26154.84112368 +.00000000 +00000-0 +33455-3 0 00007
2 39152 97.7920 245.7232 0012782 141.4420 218.7716 14.96336034 08
| Epoch (UTC): | 03 June 2026 20:11:13 |
| Eccentricity: | 0.0012782 |
| inclination: | 97.7920° |
| perigee height: | 569 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 245.7232° |
| argument of perigee: | 141.4420° |
| revolutions per day: | 14.96336034 |
| mean anomaly at epoch: | 218.7716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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