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 63385U 26145.26545344 +.00000000 +00000-0 +72585-3 0 00009
2 63385 53.1580 67.4208 0001074 91.0942 269.0182 15.30220618 09
| Epoch (UTC): | 25 May 2026 06:22:15 |
| Eccentricity: | 0.0001074 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 67.4208° |
| argument of perigee: | 91.0942° |
| revolutions per day: | 15.30220618 |
| mean anomaly at epoch: | 269.0182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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