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 68048U 26145.46976980 +.00000000 +00000-0 +91105-3 0 00005
2 68048 53.1599 51.8236 0001247 87.7604 272.3542 15.34417717 06
| Epoch (UTC): | 25 May 2026 11:16:28 |
| Eccentricity: | 0.0001247 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 51.8236° |
| argument of perigee: | 87.7604° |
| revolutions per day: | 15.34417717 |
| mean anomaly at epoch: | 272.3542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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