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 48157U 26145.50122382 +.00000000 +00000-0 +28032-4 0 00008
2 48157 99.5277 159.3318 0046838 145.5721 214.8479 13.77599349 02
| Epoch (UTC): | 25 May 2026 12:01:45 |
| Eccentricity: | 0.0046838 |
| inclination: | 99.5277° |
| perigee height: | 938 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 159.3318° |
| argument of perigee: | 145.5721° |
| revolutions per day: | 13.77599349 |
| mean anomaly at epoch: | 214.8479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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