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 61533U 26145.57646596 +.00000000 +00000-0 +27102-5 0 00004
2 61533 53.1597 217.2073 0001062 148.6214 211.4867 15.69713842 02
| Epoch (UTC): | 25 May 2026 13:50:06 |
| Eccentricity: | 0.0001062 |
| inclination: | 53.1597° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 217.2073° |
| argument of perigee: | 148.6214° |
| revolutions per day: | 15.69713842 |
| mean anomaly at epoch: | 211.4867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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