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 63838U 26145.30369595 +.00000000 +00000-0 +68535-3 0 00009
2 63838 43.0025 1.3858 0001489 279.2243 80.8440 15.27581630 02
| Epoch (UTC): | 25 May 2026 07:17:19 |
| Eccentricity: | 0.0001489 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 1.3858° |
| argument of perigee: | 279.2243° |
| revolutions per day: | 15.27581630 |
| mean anomaly at epoch: | 80.8440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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