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 48243U 26145.40074705 +.00000000 +00000-0 +67562-3 0 00008
2 48243 87.8944 294.2495 0001478 103.6880 256.4414 13.14501837 03
| Epoch (UTC): | 25 May 2026 09:37:04 |
| Eccentricity: | 0.0001478 |
| inclination: | 87.8944° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2495° |
| argument of perigee: | 103.6880° |
| revolutions per day: | 13.14501837 |
| mean anomaly at epoch: | 256.4414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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