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 50829U 26145.47128926 +.00000000 +00000-0 -17068-3 0 00000
2 50829 53.2114 184.4359 0001255 93.7117 266.4018 15.08846502 03
| Epoch (UTC): | 25 May 2026 11:18:39 |
| Eccentricity: | 0.0001255 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 184.4359° |
| argument of perigee: | 93.7117° |
| revolutions per day: | 15.08846502 |
| mean anomaly at epoch: | 266.4018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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