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 62403U 26145.40294995 +.00000000 +00000-0 +48280-3 0 00003
2 62403 45.0047 42.4814 0003808 155.9567 204.1499 15.37964691 07
| Epoch (UTC): | 25 May 2026 09:40:14 |
| Eccentricity: | 0.0003808 |
| inclination: | 45.0047° |
| perigee height: | 450 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 42.4814° |
| argument of perigee: | 155.9567° |
| revolutions per day: | 15.37964691 |
| mean anomaly at epoch: | 204.1499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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