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 68999U 26145.26782723 +.00000000 +00000-0 +13336-3 0 00008
2 68999 97.7366 43.1457 0002115 185.7373 174.3822 14.91820333 09
| Epoch (UTC): | 25 May 2026 06:25:40 |
| Eccentricity: | 0.0002115 |
| inclination: | 97.7366° |
| perigee height: | 591 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 43.1457° |
| argument of perigee: | 185.7373° |
| revolutions per day: | 14.91820333 |
| mean anomaly at epoch: | 174.3822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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