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 68634U 26145.03669363 +.00000000 +00000-0 +30006-3 0 00006
2 68634 60.0204 266.5784 0026003 17.7602 342.4382 15.25974840 04
| Epoch (UTC): | 25 May 2026 00:52:50 |
| Eccentricity: | 0.0026003 |
| inclination: | 60.0204° |
| perigee height: | 470 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 266.5784° |
| argument of perigee: | 17.7602° |
| revolutions per day: | 15.25974840 |
| mean anomaly at epoch: | 342.4382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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