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 48231U 26145.37379023 +.00000000 +00000-0 -22972-3 0 00009
2 48231 87.8934 294.2762 0001857 99.6633 260.4706 13.14503146 01
| Epoch (UTC): | 25 May 2026 08:58:15 |
| Eccentricity: | 0.0001857 |
| inclination: | 87.8934° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2762° |
| argument of perigee: | 99.6633° |
| revolutions per day: | 13.14503146 |
| mean anomaly at epoch: | 260.4706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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