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 60462U 26145.60048433 +.00000000 +00000-0 +47370-3 0 00001
2 60462 34.9928 302.2556 0005296 10.1708 349.9114 15.23078076 07
| Epoch (UTC): | 25 May 2026 14:24:41 |
| Eccentricity: | 0.0005296 |
| inclination: | 34.9928° |
| perigee height: | 493 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 302.2556° |
| argument of perigee: | 10.1708° |
| revolutions per day: | 15.23078076 |
| mean anomaly at epoch: | 349.9114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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