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 54013U 26145.46254441 +.00000000 +00000-0 +42495-5 0 00003
2 54013 53.2122 219.4299 0000892 87.5730 272.5365 15.08843588 05
| Epoch (UTC): | 25 May 2026 11:06:03 |
| Eccentricity: | 0.0000892 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 219.4299° |
| argument of perigee: | 87.5730° |
| revolutions per day: | 15.08843588 |
| mean anomaly at epoch: | 272.5365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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