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 68871U 26145.58646898 +.00000000 +00000-0 +73718-3 0 00004
2 68871 51.8827 351.5680 0003229 197.4624 162.6253 15.38197940 02
| Epoch (UTC): | 25 May 2026 14:04:30 |
| Eccentricity: | 0.0003229 |
| inclination: | 51.8827° |
| perigee height: | 449 km |
| apogee height: | 454 km |
| right ascension of ascending node: | 351.5680° |
| argument of perigee: | 197.4624° |
| revolutions per day: | 15.38197940 |
| mean anomaly at epoch: | 162.6253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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