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 39410U 26145.65333227 +.00000000 +00000-0 -49338-3 0 00000
2 39410 100.1106 123.0596 0009794 135.9784 224.2111 13.15582045 07
| Epoch (UTC): | 25 May 2026 15:40:47 |
| Eccentricity: | 0.0009794 |
| inclination: | 100.1106° |
| perigee height: | 1194 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 123.0596° |
| argument of perigee: | 135.9784° |
| revolutions per day: | 13.15582045 |
| mean anomaly at epoch: | 224.2111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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