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 68415U 26145.29971786 +.00000000 +00000-0 +22248-3 0 00005
2 68415 84.9667 242.2937 0024231 337.8447 22.1727 14.88576399 04
| Epoch (UTC): | 25 May 2026 07:11:35 |
| Eccentricity: | 0.0024231 |
| inclination: | 84.9667° |
| perigee height: | 585 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 242.2937° |
| argument of perigee: | 337.8447° |
| revolutions per day: | 14.88576399 |
| mean anomaly at epoch: | 22.1727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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