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 62735U 26145.50792338 +.00000000 +00000-0 +77159-3 0 00003
2 62735 42.9994 80.7441 0000670 242.3714 117.7069 15.27588147 01
| Epoch (UTC): | 25 May 2026 12:11:24 |
| Eccentricity: | 0.0000670 |
| inclination: | 42.9994° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 80.7441° |
| argument of perigee: | 242.3714° |
| revolutions per day: | 15.27588147 |
| mean anomaly at epoch: | 117.7069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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