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 49298U 26145.35936912 +.00000000 +00000-0 +11809-3 0 00003
2 49298 87.9177 278.9929 0001840 98.6155 261.5187 13.20770147 08
| Epoch (UTC): | 25 May 2026 08:37:29 |
| Eccentricity: | 0.0001840 |
| inclination: | 87.9177° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9929° |
| argument of perigee: | 98.6155° |
| revolutions per day: | 13.20770147 |
| mean anomaly at epoch: | 261.5187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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