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 60918U 26145.64750218 +.00000000 +00000-0 +95013-7 0 00003
2 60918 53.1622 286.6576 0001170 111.8709 248.2416 15.30189720 04
| Epoch (UTC): | 25 May 2026 15:32:24 |
| Eccentricity: | 0.0001170 |
| inclination: | 53.1622° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 286.6576° |
| argument of perigee: | 111.8709° |
| revolutions per day: | 15.30189720 |
| mean anomaly at epoch: | 248.2416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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