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 48985U 26145.49366604 +.00000000 +00000-0 -51460-4 0 00004
2 48985 87.9106 233.2768 0001877 94.9151 265.2194 13.16593244 07
| Epoch (UTC): | 25 May 2026 11:50:52 |
| Eccentricity: | 0.0001877 |
| inclination: | 87.9106° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2768° |
| argument of perigee: | 94.9151° |
| revolutions per day: | 13.16593244 |
| mean anomaly at epoch: | 265.2194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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