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 49288U 26145.43218720 +.00000000 +00000-0 +56181-4 0 00004
2 49288 87.9151 309.5146 0001565 98.6618 261.4692 13.19726653 00
| Epoch (UTC): | 25 May 2026 10:22:20 |
| Eccentricity: | 0.0001565 |
| inclination: | 87.9151° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5146° |
| argument of perigee: | 98.6618° |
| revolutions per day: | 13.19726653 |
| mean anomaly at epoch: | 261.4692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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