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 49954U 26145.66668980 +.00000000 +00000-0 +58428-3 0 00001
2 49954 0.2300 127.5632 0006724 99.4082 202.4004 15.10009634 06
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0006724 |
| inclination: | 0.2300° |
| perigee height: | 532 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 127.5632° |
| argument of perigee: | 99.4082° |
| revolutions per day: | 15.10009634 |
| mean anomaly at epoch: | 202.4004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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