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 58272U 26145.54241257 +.00000000 +00000-0 +99062-3 0 00004
2 58272 97.3747 244.4235 0009054 243.6254 116.4096 16.02016807 09
| Epoch (UTC): | 25 May 2026 13:01:04 |
| Eccentricity: | 0.0009054 |
| inclination: | 97.3747° |
| perigee height: | 263 km |
| apogee height: | 275 km |
| right ascension of ascending node: | 244.4235° |
| argument of perigee: | 243.6254° |
| revolutions per day: | 16.02016807 |
| mean anomaly at epoch: | 116.4096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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