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 50839U 26145.52188705 +.00000000 +00000-0 -54378-4 0 00004
2 50839 53.2111 194.2051 0001034 90.4765 269.6346 15.08845840 00
| Epoch (UTC): | 25 May 2026 12:31:31 |
| Eccentricity: | 0.0001034 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 194.2051° |
| argument of perigee: | 90.4765° |
| revolutions per day: | 15.08845840 |
| mean anomaly at epoch: | 269.6346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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