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 61203U 26145.44424493 +.00000000 +00000-0 +67999-5 0 00002
2 61203 53.1589 157.9059 0001026 69.5923 290.5205 15.69696403 06
| Epoch (UTC): | 25 May 2026 10:39:42 |
| Eccentricity: | 0.0001026 |
| inclination: | 53.1589° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 157.9059° |
| argument of perigee: | 69.5923° |
| revolutions per day: | 15.69696403 |
| mean anomaly at epoch: | 290.5205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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