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 38773U 12048P 26010.74396602 0.00000000 00000-0 00000-0 0 02
2 38773 63.4204 250.4405 0296851 358.4712 1.5287 13.40991696 01
| Epoch (UTC): | 10 January 2026 17:51:18 |
| Eccentricity: | 0.0296851 |
| inclination: | 63.4204° |
| perigee height: | 883 km |
| apogee height: | 1328 km |
| right ascension of ascending node: | 250.4405° |
| argument of perigee: | 358.4712° |
| revolutions per day: | 13.40991696 |
| mean anomaly at epoch: | 1.5287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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