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 26099A 26121.79633588 .00023172 00000+0 30787-4 0 03
2 72001 53.1614 28.2468 0010628 263.2450 357.9483 16.05826900 18
| Epoch (UTC): | 01 May 2026 19:06:43 |
| Eccentricity: | 0.0010628 |
| inclination: | 53.1614° |
| perigee height: | 251 km |
| apogee height: | 265 km |
| right ascension of ascending node: | 28.2468° |
| argument of perigee: | 263.2450° |
| revolutions per day: | 16.05826900 |
| mean anomaly at epoch: | 357.9483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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