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 66238U 26145.41474648 +.00000000 +00000-0 +11146-2 0 00009
2 66238 53.1582 286.0859 0001009 99.5079 260.6038 15.34424783 04
| Epoch (UTC): | 25 May 2026 09:57:14 |
| Eccentricity: | 0.0001009 |
| inclination: | 53.1582° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 286.0859° |
| argument of perigee: | 99.5079° |
| revolutions per day: | 15.34424783 |
| mean anomaly at epoch: | 260.6038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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