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 68712U 26145.40771595 +.00000000 +00000-0 +92820-3 0 00007
2 68712 53.1602 38.1078 0000967 98.1288 261.9831 15.49331484 00
| Epoch (UTC): | 25 May 2026 09:47:06 |
| Eccentricity: | 0.0000967 |
| inclination: | 53.1602° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 38.1078° |
| argument of perigee: | 98.1288° |
| revolutions per day: | 15.49331484 |
| mean anomaly at epoch: | 261.9831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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