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 00005U 26131.85922292 +.00000000 +00000-0 +13340-3 0 00004
2 00005 34.2500 66.4383 1836232 334.6666 17.3922 10.85980560 06
| Epoch (UTC): | 11 May 2026 20:37:16 |
| Eccentricity: | 0.1836232 |
| inclination: | 34.2500° |
| perigee height: | 654 km |
| apogee height: | 3817 km |
| right ascension of ascending node: | 66.4383° |
| argument of perigee: | 334.6666° |
| revolutions per day: | 10.85980560 |
| mean anomaly at epoch: | 17.3922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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