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 63003U 26145.12642112 +.00000000 +00000-0 +46065-3 0 00006
2 63003 97.3173 221.3663 0004182 72.9671 287.2027 15.29046883 08
| Epoch (UTC): | 25 May 2026 03:02:02 |
| Eccentricity: | 0.0004182 |
| inclination: | 97.3173° |
| perigee height: | 476 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 221.3663° |
| argument of perigee: | 72.9671° |
| revolutions per day: | 15.29046883 |
| mean anomaly at epoch: | 287.2027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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