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 48436U 26145.37363068 +.00000000 +00000-0 +49681-4 0 00004
2 48436 53.1589 181.4893 0001249 88.8922 271.2222 15.31699436 00
| Epoch (UTC): | 25 May 2026 08:58:01 |
| Eccentricity: | 0.0001249 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 181.4893° |
| argument of perigee: | 88.8922° |
| revolutions per day: | 15.31699436 |
| mean anomaly at epoch: | 271.2222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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