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 26040.34425014 +.00000000 +00000-0 +25644-3 0 00000
2 00053 47.2794 16.6938 0098114 57.1096 303.9088 12.17401147 06
| Epoch (UTC): | 09 February 2026 08:15:43 |
| Eccentricity: | 0.0098114 |
| inclination: | 47.2794° |
| perigee height: | 1526 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 16.6938° |
| argument of perigee: | 57.1096° |
| revolutions per day: | 12.17401147 |
| mean anomaly at epoch: | 303.9088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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