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 66837U 26145.41346450 +.00000000 +00000-0 +75482-3 0 00007
2 66837 70.0009 141.1997 0003740 268.9700 91.1031 14.98346153 05
| Epoch (UTC): | 25 May 2026 09:55:23 |
| Eccentricity: | 0.0003740 |
| inclination: | 70.0009° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.1997° |
| argument of perigee: | 268.9700° |
| revolutions per day: | 14.98346153 |
| mean anomaly at epoch: | 91.1031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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