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 62038U 26145.52162602 +.00000000 +00000-0 +12219-2 0 00001
2 62038 42.9888 160.8506 0021953 96.5880 263.7485 15.63884898 07
| Epoch (UTC): | 25 May 2026 12:31:08 |
| Eccentricity: | 0.0021953 |
| inclination: | 42.9888° |
| perigee height: | 362 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 160.8506° |
| argument of perigee: | 96.5880° |
| revolutions per day: | 15.63884898 |
| mean anomaly at epoch: | 263.7485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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