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 60088U 26145.61070247 +.00000000 +00000-0 +17015-3 0 00007
2 60088 28.9952 254.0284 0004014 191.0817 168.9689 14.84836811 01
| Epoch (UTC): | 25 May 2026 14:39:24 |
| Eccentricity: | 0.0004014 |
| inclination: | 28.9952° |
| perigee height: | 611 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 254.0284° |
| argument of perigee: | 191.0817° |
| revolutions per day: | 14.84836811 |
| mean anomaly at epoch: | 168.9689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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