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 60318U 26144.72733404 +.00000000 +00000-0 -99366-4 0 00006
2 60318 53.1618 303.7568 0001203 83.9574 276.1563 15.30198147 07
| Epoch (UTC): | 24 May 2026 17:27:21 |
| Eccentricity: | 0.0001203 |
| inclination: | 53.1618° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 303.7568° |
| argument of perigee: | 83.9574° |
| revolutions per day: | 15.30198147 |
| mean anomaly at epoch: | 276.1563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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