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 60152U 26145.66668980 +.00000000 +00000-0 -27316-3 0 00007
2 60152 53.1599 322.5687 0001177 87.0474 105.5437 15.33551906 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.1599° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 322.5687° |
| argument of perigee: | 87.0474° |
| revolutions per day: | 15.33551906 |
| mean anomaly at epoch: | 105.5437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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