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 39260U 26145.64026075 +.00000000 +00000-0 +52863-4 0 00009
2 39260 98.4969 120.5525 0015880 88.3137 271.9857 14.15749001 00
| Epoch (UTC): | 25 May 2026 15:21:58 |
| Eccentricity: | 0.0015880 |
| inclination: | 98.4969° |
| perigee height: | 828 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 120.5525° |
| argument of perigee: | 88.3137° |
| revolutions per day: | 14.15749001 |
| mean anomaly at epoch: | 271.9857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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