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 48692U 26145.52085318 +.00000000 +00000-0 +70137-5 0 00005
2 48692 53.1604 77.7509 0001186 85.7368 274.3769 15.31698789 03
| Epoch (UTC): | 25 May 2026 12:30:01 |
| Eccentricity: | 0.0001186 |
| inclination: | 53.1604° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 77.7509° |
| argument of perigee: | 85.7368° |
| revolutions per day: | 15.31698789 |
| mean anomaly at epoch: | 274.3769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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