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 39070U 26145.59132580 +.00000000 +00000-0 +00000-0 0 00003
2 39070 3.4881 30.8751 0005164 16.3282 234.4601 1.00274795 02
| Epoch (UTC): | 25 May 2026 14:11:30 |
| Eccentricity: | 0.0005164 |
| inclination: | 3.4881° |
| perigee height: | 35764 km |
| apogee height: | 35808 km |
| right ascension of ascending node: | 30.8751° |
| argument of perigee: | 16.3282° |
| revolutions per day: | 1.00274795 |
| mean anomaly at epoch: | 234.4601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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