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 60415U 26144.99467211 +.00000000 +00000-0 -74166-6 0 00006
2 60415 53.1613 247.4201 0000927 106.2109 253.8996 15.34392083 04
| Epoch (UTC): | 24 May 2026 23:52:19 |
| Eccentricity: | 0.0000927 |
| inclination: | 53.1613° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 247.4201° |
| argument of perigee: | 106.2109° |
| revolutions per day: | 15.34392083 |
| mean anomaly at epoch: | 253.8996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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