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 39160U 26145.61579323 +.00000000 +00000-0 +14852-3 0 00009
2 39160 97.9092 199.8977 0001505 96.6248 263.5127 14.64829656 00
| Epoch (UTC): | 25 May 2026 14:46:44 |
| Eccentricity: | 0.0001505 |
| inclination: | 97.9092° |
| perigee height: | 677 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 199.8977° |
| argument of perigee: | 96.6248° |
| revolutions per day: | 14.64829656 |
| mean anomaly at epoch: | 263.5127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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