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 39444U 26102.67584860 +.00000000 +00000-0 +37539-3 0 00002
2 39444 97.8222 72.8193 0038673 67.9052 292.6275 15.08561186 06
| Epoch (UTC): | 12 April 2026 16:13:13 |
| Eccentricity: | 0.0038673 |
| inclination: | 97.8222° |
| perigee height: | 514 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 72.8193° |
| argument of perigee: | 67.9052° |
| revolutions per day: | 15.08561186 |
| mean anomaly at epoch: | 292.6275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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