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 60095U 26145.09151882 +.00000000 +00000-0 +51969-4 0 00009
2 60095 53.1621 42.2655 0001136 102.2370 257.8758 15.30194730 05
| Epoch (UTC): | 25 May 2026 02:11:47 |
| Eccentricity: | 0.0001136 |
| inclination: | 53.1621° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 42.2655° |
| argument of perigee: | 102.2370° |
| revolutions per day: | 15.30194730 |
| mean anomaly at epoch: | 257.8758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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