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 68883U 26145.59552683 +.00000000 +00000-0 +73463-3 0 00003
2 68883 51.8806 351.6239 0005696 203.7099 156.3626 15.37711154 02
| Epoch (UTC): | 25 May 2026 14:17:33 |
| Eccentricity: | 0.0005696 |
| inclination: | 51.8806° |
| perigee height: | 449 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 351.6239° |
| argument of perigee: | 203.7099° |
| revolutions per day: | 15.37711154 |
| mean anomaly at epoch: | 156.3626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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