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 50491U 26145.25590071 +.00000000 +00000-0 +24778-3 0 00000
2 50491 87.9169 340.0004 0001971 85.2170 274.9188 13.18687984 07
| Epoch (UTC): | 25 May 2026 06:08:29 |
| Eccentricity: | 0.0001971 |
| inclination: | 87.9169° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0004° |
| argument of perigee: | 85.2170° |
| revolutions per day: | 13.18687984 |
| mean anomaly at epoch: | 274.9188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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