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 60505U 26144.81678302 +.00000000 +00000-0 +40585-3 0 00006
2 60505 97.3712 228.9635 0003510 34.6753 325.4723 15.42074045 07
| Epoch (UTC): | 24 May 2026 19:36:10 |
| Eccentricity: | 0.0003510 |
| inclination: | 97.3712° |
| perigee height: | 438 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 228.9635° |
| argument of perigee: | 34.6753° |
| revolutions per day: | 15.42074045 |
| mean anomaly at epoch: | 325.4723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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