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 50502U 26145.29390456 +.00000000 +00000-0 -40492-4 0 00005
2 50502 87.9169 339.9864 0001608 107.6762 252.4545 13.18712729 08
| Epoch (UTC): | 25 May 2026 07:03:13 |
| Eccentricity: | 0.0001608 |
| inclination: | 87.9169° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9864° |
| argument of perigee: | 107.6762° |
| revolutions per day: | 13.18712729 |
| mean anomaly at epoch: | 252.4545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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