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 00050U 26157.80115817 +.00000000 +00000-0 +13453-3 0 00009
2 00050 47.2284 193.9659 0113469 343.5610 16.1515 12.20165824 02
| Epoch (UTC): | 06 June 2026 19:13:40 |
| Eccentricity: | 0.0113469 |
| inclination: | 47.2284° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 193.9659° |
| argument of perigee: | 343.5610° |
| revolutions per day: | 12.20165824 |
| mean anomaly at epoch: | 16.1515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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