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 61003U 26145.51992814 +.00000000 +00000-0 +10629-3 0 00001
2 61003 53.1600 68.7077 0001256 90.8349 269.2795 15.30179194 09
| Epoch (UTC): | 25 May 2026 12:28:41 |
| Eccentricity: | 0.0001256 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 68.7077° |
| argument of perigee: | 90.8349° |
| revolutions per day: | 15.30179194 |
| mean anomaly at epoch: | 269.2795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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