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 66870U 26145.64973466 +.00000000 +00000-0 +71505-3 0 00004
2 66870 42.9994 269.0083 0001236 273.5835 86.4875 15.27592452 09
| Epoch (UTC): | 25 May 2026 15:35:37 |
| Eccentricity: | 0.0001236 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 269.0083° |
| argument of perigee: | 273.5835° |
| revolutions per day: | 15.27592452 |
| mean anomaly at epoch: | 86.4875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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