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 48990U 26145.24192816 +.00000000 +00000-0 +17316-3 0 00005
2 48990 87.9107 233.3405 0002079 91.7516 268.3853 13.16595367 02
| Epoch (UTC): | 25 May 2026 05:48:22 |
| Eccentricity: | 0.0002079 |
| inclination: | 87.9107° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.3405° |
| argument of perigee: | 91.7516° |
| revolutions per day: | 13.16595367 |
| mean anomaly at epoch: | 268.3853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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