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 52754U 26145.39809111 +.00000000 +00000-0 +32316-3 0 00004
2 52754 97.6568 303.6179 0005446 148.0912 212.0670 15.50458135 04
| Epoch (UTC): | 25 May 2026 09:33:15 |
| Eccentricity: | 0.0005446 |
| inclination: | 97.6568° |
| perigee height: | 412 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 303.6179° |
| argument of perigee: | 148.0912° |
| revolutions per day: | 15.50458135 |
| mean anomaly at epoch: | 212.0670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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