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 60035U 26145.51353433 +.00000000 +00000-0 +16503-3 0 00000
2 60035 53.1618 78.9183 0001303 68.3229 291.7911 15.30225551 02
| Epoch (UTC): | 25 May 2026 12:19:29 |
| Eccentricity: | 0.0001303 |
| inclination: | 53.1618° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.9183° |
| argument of perigee: | 68.3229° |
| revolutions per day: | 15.30225551 |
| mean anomaly at epoch: | 291.7911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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