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 49204U 26145.38981697 +.00000000 +00000-0 +18695-3 0 00003
2 49204 87.9164 278.9959 0001624 92.5244 267.6075 13.20773583 06
| Epoch (UTC): | 25 May 2026 09:21:20 |
| Eccentricity: | 0.0001624 |
| inclination: | 87.9164° |
| perigee height: | 1181 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9959° |
| argument of perigee: | 92.5244° |
| revolutions per day: | 13.20773583 |
| mean anomaly at epoch: | 267.6075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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