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 62994U 26145.14517963 +.00000000 +00000-0 +66637-3 0 00008
2 62994 42.9984 71.9408 0001307 264.7102 95.3601 15.27601236 07
| Epoch (UTC): | 25 May 2026 03:29:03 |
| Eccentricity: | 0.0001307 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 71.9408° |
| argument of perigee: | 264.7102° |
| revolutions per day: | 15.27601236 |
| mean anomaly at epoch: | 95.3601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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