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 50487U 26145.50545567 +.00000000 +00000-0 +38715-4 0 00000
2 50487 87.9168 339.9617 0001659 83.8059 276.3262 13.18685164 08
| Epoch (UTC): | 25 May 2026 12:07:51 |
| Eccentricity: | 0.0001659 |
| inclination: | 87.9168° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9617° |
| argument of perigee: | 83.8059° |
| revolutions per day: | 13.18685164 |
| mean anomaly at epoch: | 276.3262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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