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 60272U 26145.05786956 +.00000000 +00000-0 -37015-4 0 00005
2 60272 53.1600 57.5151 0001016 102.8278 257.2837 15.30184711 09
| Epoch (UTC): | 25 May 2026 01:23:19 |
| Eccentricity: | 0.0001016 |
| inclination: | 53.1600° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.5151° |
| argument of perigee: | 102.8278° |
| revolutions per day: | 15.30184711 |
| mean anomaly at epoch: | 257.2837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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