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 68061U 26145.15241372 +.00000000 +00000-0 +13453-2 0 00005
2 68061 53.1583 52.6798 0000373 52.8867 307.2170 15.34400231 07
| Epoch (UTC): | 25 May 2026 03:39:28 |
| Eccentricity: | 0.0000373 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 52.6798° |
| argument of perigee: | 52.8867° |
| revolutions per day: | 15.34400231 |
| mean anomaly at epoch: | 307.2170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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