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 63704U 26145.50026536 +.00000000 +00000-0 +20285-3 0 00008
2 63704 53.1580 222.4958 0001218 88.9500 271.1641 15.30203446 08
| Epoch (UTC): | 25 May 2026 12:00:22 |
| Eccentricity: | 0.0001218 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.4958° |
| argument of perigee: | 88.9500° |
| revolutions per day: | 15.30203446 |
| mean anomaly at epoch: | 271.1641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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