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 49049U 26145.60233953 +.00000000 +00000-0 +21318-3 0 00006
2 49049 97.2777 214.3850 0000367 100.0714 260.0565 15.23484630 09
| Epoch (UTC): | 25 May 2026 14:27:22 |
| Eccentricity: | 0.0000367 |
| inclination: | 97.2777° |
| perigee height: | 495 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 214.3850° |
| argument of perigee: | 100.0714° |
| revolutions per day: | 15.23484630 |
| mean anomaly at epoch: | 260.0565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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