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 68870U 26145.60385051 +.00000000 +00000-0 +10682-2 0 00007
2 68870 51.8806 351.6770 0007704 208.4491 151.6076 15.37200804 00
| Epoch (UTC): | 25 May 2026 14:29:32 |
| Eccentricity: | 0.0007704 |
| inclination: | 51.8806° |
| perigee height: | 449 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 351.6770° |
| argument of perigee: | 208.4491° |
| revolutions per day: | 15.37200804 |
| mean anomaly at epoch: | 151.6076° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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