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 68340U 26145.00002315 +.00000000 +00000-0 +19557-2 0 00002
2 68340 53.1592 349.7800 0000951 84.7574 346.5556 15.35369227 06
| Epoch (UTC): | 25 May 2026 00:00:02 |
| Eccentricity: | 0.0000951 |
| inclination: | 53.1592° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 349.7800° |
| argument of perigee: | 84.7574° |
| revolutions per day: | 15.35369227 |
| mean anomaly at epoch: | 346.5556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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