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 60308U 26145.33401567 +.00000000 +00000-0 +12789-4 0 00008
2 60308 53.1588 128.2658 0001143 62.1668 297.9466 15.69707077 01
| Epoch (UTC): | 25 May 2026 08:00:58 |
| Eccentricity: | 0.0001143 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 128.2658° |
| argument of perigee: | 62.1668° |
| revolutions per day: | 15.69707077 |
| mean anomaly at epoch: | 297.9466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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