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 62134U 26145.04015624 +.00000000 +00000-0 +51705-3 0 00000
2 62134 42.9997 61.7206 0000560 250.2120 109.8671 15.27574481 09
| Epoch (UTC): | 25 May 2026 00:57:49 |
| Eccentricity: | 0.0000560 |
| inclination: | 42.9997° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 61.7206° |
| argument of perigee: | 250.2120° |
| revolutions per day: | 15.27574481 |
| mean anomaly at epoch: | 109.8671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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