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 60028U 26145.09950339 +.00000000 +00000-0 +14939-4 0 00005
2 60028 53.1603 80.6000 0001346 66.4249 293.6893 15.30193884 07
| Epoch (UTC): | 25 May 2026 02:23:17 |
| Eccentricity: | 0.0001346 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.6000° |
| argument of perigee: | 66.4249° |
| revolutions per day: | 15.30193884 |
| mean anomaly at epoch: | 293.6893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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