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 49291U 26145.36585551 +.00000000 +00000-0 -31519-4 0 00008
2 49291 87.9160 309.5145 0001718 92.6399 267.4930 13.19726532 00
| Epoch (UTC): | 25 May 2026 08:46:49 |
| Eccentricity: | 0.0001718 |
| inclination: | 87.9160° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5145° |
| argument of perigee: | 92.6399° |
| revolutions per day: | 13.19726532 |
| mean anomaly at epoch: | 267.4930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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