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 26088.11835905 +.00000000 +00000-0 +88634-3 0 00009
2 00053 47.2766 229.3244 0100176 198.5297 161.1830 12.17407350 04
| Epoch (UTC): | 29 March 2026 02:50:26 |
| Eccentricity: | 0.0100176 |
| inclination: | 47.2766° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 229.3244° |
| argument of perigee: | 198.5297° |
| revolutions per day: | 12.17407350 |
| mean anomaly at epoch: | 161.1830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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