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 50494U 26145.06492135 +.00000000 +00000-0 -71564-5 0 00002
2 50494 87.9171 340.0571 0001852 96.9411 263.1932 13.18664070 05
| Epoch (UTC): | 25 May 2026 01:33:29 |
| Eccentricity: | 0.0001852 |
| inclination: | 87.9171° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0571° |
| argument of perigee: | 96.9411° |
| revolutions per day: | 13.18664070 |
| mean anomaly at epoch: | 263.1932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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