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 63258U 26145.26803608 +.00000000 +00000-0 +13674-3 0 00002
2 63258 97.6920 37.6000 0001724 86.6522 273.4896 14.95203427 04
| Epoch (UTC): | 25 May 2026 06:25:58 |
| Eccentricity: | 0.0001724 |
| inclination: | 97.6920° |
| perigee height: | 581 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 37.6000° |
| argument of perigee: | 86.6522° |
| revolutions per day: | 14.95203427 |
| mean anomaly at epoch: | 273.4896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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