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 61675U 26145.25901506 +.00000000 +00000-0 +58715-4 0 00004
2 61675 53.1618 95.0743 0001293 82.4281 277.6867 15.31702262 01
| Epoch (UTC): | 25 May 2026 06:12:58 |
| Eccentricity: | 0.0001293 |
| inclination: | 53.1618° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.0743° |
| argument of perigee: | 82.4281° |
| revolutions per day: | 15.31702262 |
| mean anomaly at epoch: | 277.6867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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