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 50804U 26145.46116409 +.00000000 +00000-0 -15073-3 0 00009
2 50804 53.2112 174.4810 0001150 91.8164 268.2960 15.08854919 07
| Epoch (UTC): | 25 May 2026 11:04:04 |
| Eccentricity: | 0.0001150 |
| inclination: | 53.2112° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 174.4810° |
| argument of perigee: | 91.8164° |
| revolutions per day: | 15.08854919 |
| mean anomaly at epoch: | 268.2960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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