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 48864U 26145.56483453 +.00000000 +00000-0 +28173-3 0 00003
2 48864 34.9985 218.6644 0004449 124.3209 235.7925 15.13335525 09
| Epoch (UTC): | 25 May 2026 13:33:21 |
| Eccentricity: | 0.0004449 |
| inclination: | 34.9985° |
| perigee height: | 523 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 218.6644° |
| argument of perigee: | 124.3209° |
| revolutions per day: | 15.13335525 |
| mean anomaly at epoch: | 235.7925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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