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 48023U 26145.54192831 +.00000000 +00000-0 +12448-2 0 00002
2 48023 53.1197 331.5772 0002191 210.0838 150.0042 15.41069073 06
| Epoch (UTC): | 25 May 2026 13:00:22 |
| Eccentricity: | 0.0002191 |
| inclination: | 53.1197° |
| perigee height: | 441 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 331.5772° |
| argument of perigee: | 210.0838° |
| revolutions per day: | 15.41069073 |
| mean anomaly at epoch: | 150.0042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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