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 48073U 26145.46124465 +.00000000 +00000-0 -32710-3 0 00002
2 48073 87.8950 324.7294 0001525 83.7265 276.4037 13.13469472 05
| Epoch (UTC): | 25 May 2026 11:04:11 |
| Eccentricity: | 0.0001525 |
| inclination: | 87.8950° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7294° |
| argument of perigee: | 83.7265° |
| revolutions per day: | 13.13469472 |
| mean anomaly at epoch: | 276.4037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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