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 52344U 26145.48693414 +.00000000 +00000-0 -13896-3 0 00009
2 52344 53.2105 214.4316 0001213 97.8244 262.2886 15.08849500 02
| Epoch (UTC): | 25 May 2026 11:41:11 |
| Eccentricity: | 0.0001213 |
| inclination: | 53.2105° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 214.4316° |
| argument of perigee: | 97.8244° |
| revolutions per day: | 15.08849500 |
| mean anomaly at epoch: | 262.2886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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