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 62404U 26145.01213625 +.00000000 +00000-0 +69464-3 0 00009
2 62404 44.9961 21.9261 0007461 168.9270 191.1787 15.49743557 07
| Epoch (UTC): | 25 May 2026 00:17:28 |
| Eccentricity: | 0.0007461 |
| inclination: | 44.9961° |
| perigee height: | 412 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 21.9261° |
| argument of perigee: | 168.9270° |
| revolutions per day: | 15.49743557 |
| mean anomaly at epoch: | 191.1787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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