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 39504U 26145.50439168 +.00000000 +00000-0 +00000-0 0 00008
2 39504 3.9560 18.7335 0002330 216.6473 148.3440 1.00275193 02
| Epoch (UTC): | 25 May 2026 12:06:19 |
| Eccentricity: | 0.0002330 |
| inclination: | 3.9560° |
| perigee height: | 35776 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 18.7335° |
| argument of perigee: | 216.6473° |
| revolutions per day: | 1.00275193 |
| mean anomaly at epoch: | 148.3440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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