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 00053U 26159.86196690 +.00000000 +00000-0 +26737-3 0 00007
2 00053 47.2797 8.0135 0100570 51.3738 309.6003 12.17413519 08
| Epoch (UTC): | 08 June 2026 20:41:13 |
| Eccentricity: | 0.0100570 |
| inclination: | 47.2797° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 8.0135° |
| argument of perigee: | 51.3738° |
| revolutions per day: | 12.17413519 |
| mean anomaly at epoch: | 309.6003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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