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 68993U 26145.26953098 +.00000000 +00000-0 +15746-3 0 00004
2 68993 97.7393 43.1492 0002503 188.4171 171.7006 14.91683403 09
| Epoch (UTC): | 25 May 2026 06:28:07 |
| Eccentricity: | 0.0002503 |
| inclination: | 97.7393° |
| perigee height: | 591 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 43.1492° |
| argument of perigee: | 188.4171° |
| revolutions per day: | 14.91683403 |
| mean anomaly at epoch: | 171.7006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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