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 48771U 26145.31109471 +.00000000 +00000-0 +45680-3 0 00000
2 48771 87.8999 263.7480 0001525 92.0499 268.0806 13.15546821 01
| Epoch (UTC): | 25 May 2026 07:27:58 |
| Eccentricity: | 0.0001525 |
| inclination: | 87.8999° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7480° |
| argument of perigee: | 92.0499° |
| revolutions per day: | 13.15546821 |
| mean anomaly at epoch: | 268.0806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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