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 60267U 26145.19165834 +.00000000 +00000-0 +51045-4 0 00008
2 60267 53.1605 56.9243 0001106 97.9207 262.1919 15.30192171 04
| Epoch (UTC): | 25 May 2026 04:35:59 |
| Eccentricity: | 0.0001106 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 56.9243° |
| argument of perigee: | 97.9207° |
| revolutions per day: | 15.30192171 |
| mean anomaly at epoch: | 262.1919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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