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 60115U 26145.43079880 +.00000000 +00000-0 +46828-5 0 00006
2 60115 53.1594 203.1563 0001139 74.9343 285.1800 15.69699045 04
| Epoch (UTC): | 25 May 2026 10:20:21 |
| Eccentricity: | 0.0001139 |
| inclination: | 53.1594° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 203.1563° |
| argument of perigee: | 74.9343° |
| revolutions per day: | 15.69699045 |
| mean anomaly at epoch: | 285.1800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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