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 38735U 26141.22297817 +.00000000 +00000-0 +16399-3 0 00002
2 38735 82.4746 91.5053 0018326 123.4911 236.7923 12.42648316 02
| Epoch (UTC): | 21 May 2026 05:21:05 |
| Eccentricity: | 0.0018326 |
| inclination: | 82.4746° |
| perigee height: | 1481 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 91.5053° |
| argument of perigee: | 123.4911° |
| revolutions per day: | 12.42648316 |
| mean anomaly at epoch: | 236.7923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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