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 48230U 26145.64019832 +.00000000 +00000-0 +61996-3 0 00005
2 48230 87.8934 294.2244 0001696 103.3722 256.7596 13.14501542 01
| Epoch (UTC): | 25 May 2026 15:21:53 |
| Eccentricity: | 0.0001696 |
| inclination: | 87.8934° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2244° |
| argument of perigee: | 103.3722° |
| revolutions per day: | 13.14501542 |
| mean anomaly at epoch: | 256.7596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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