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 68278U 26145.58335647 +.00000000 +00000-0 -86709-4 0 00008
2 68278 53.1602 321.1401 0001174 116.6924 16.9572 15.35427369 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001174 |
| inclination: | 53.1602° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 321.1401° |
| argument of perigee: | 116.6924° |
| revolutions per day: | 15.35427369 |
| mean anomaly at epoch: | 16.9572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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