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 38528U 12034A 25359.90744325 0.00000000 00000-0 00000-0 0 07
2 38528 6.9537 61.2150 0041322 331.7233 28.2734 1.00271606 06
| Epoch (UTC): | 25 December 2025 21:46:43 |
| Eccentricity: | 0.0041322 |
| inclination: | 6.9537° |
| perigee height: | 35612 km |
| apogee height: | 35960 km |
| right ascension of ascending node: | 61.2150° |
| argument of perigee: | 331.7233° |
| revolutions per day: | 1.00271606 |
| mean anomaly at epoch: | 28.2734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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