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 26044.28444309 +.00000000 +00000-0 +88624-3 0 00002
2 00053 47.2799 4.5402 0098240 68.7484 292.3764 12.17401523 02
| Epoch (UTC): | 13 February 2026 06:49:35 |
| Eccentricity: | 0.0098240 |
| inclination: | 47.2799° |
| perigee height: | 1525 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 4.5402° |
| argument of perigee: | 68.7484° |
| revolutions per day: | 12.17401523 |
| mean anomaly at epoch: | 292.3764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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