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 72001C 26054A 26076.60368194 .00013638 00000+0 18980-4 0 08
2 72001 53.1610 274.0517 0008089 282.1314 343.8587 16.05133267 13
| Epoch (UTC): | 17 March 2026 14:29:18 |
| Eccentricity: | 0.0008089 |
| inclination: | 53.1610° |
| perigee height: | 255 km |
| apogee height: | 265 km |
| right ascension of ascending node: | 274.0517° |
| argument of perigee: | 282.1314° |
| revolutions per day: | 16.05133267 |
| mean anomaly at epoch: | 343.8587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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