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 62997U 26145.49381610 +.00000000 +00000-0 +65788-3 0 00003
2 62997 42.9988 69.3923 0000947 270.3811 89.6932 15.27606841 06
| Epoch (UTC): | 25 May 2026 11:51:05 |
| Eccentricity: | 0.0000947 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.3923° |
| argument of perigee: | 270.3811° |
| revolutions per day: | 15.27606841 |
| mean anomaly at epoch: | 89.6932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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