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 39362U 26039.36532846 +.00000000 +00000-0 +70414-3 0 00002
2 39362 49.5639 33.7068 5126558 109.6643 311.0989 5.38666026 02
| Epoch (UTC): | 08 February 2026 08:46:04 |
| Eccentricity: | 0.5126558 |
| inclination: | 49.5639° |
| perigee height: | 321 km |
| apogee height: | 14415 km |
| right ascension of ascending node: | 33.7068° |
| argument of perigee: | 109.6643° |
| revolutions per day: | 5.38666026 |
| mean anomaly at epoch: | 311.0989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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