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 53467U 26145.66668980 +.00000000 +00000-0 +79212-2 0 00008
2 53467 97.6051 268.9430 0001514 79.1526 272.4128 15.43965301 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001514 |
| inclination: | 97.6051° |
| perigee height: | 433 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 268.9430° |
| argument of perigee: | 79.1526° |
| revolutions per day: | 15.43965301 |
| mean anomaly at epoch: | 272.4128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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