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 66270U 26145.40196418 +.00000000 +00000-0 +83632-3 0 00000
2 66270 53.1601 194.0659 0001072 55.4114 304.6990 15.34412278 01
| Epoch (UTC): | 25 May 2026 09:38:49 |
| Eccentricity: | 0.0001072 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 194.0659° |
| argument of perigee: | 55.4114° |
| revolutions per day: | 15.34412278 |
| mean anomaly at epoch: | 304.6990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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