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 54074U 26145.29138714 +.00000000 +00000-0 +18749-3 0 00008
2 54074 53.2126 359.8562 0001575 92.5116 267.6057 15.08823014 06
| Epoch (UTC): | 25 May 2026 06:59:35 |
| Eccentricity: | 0.0001575 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 359.8562° |
| argument of perigee: | 92.5116° |
| revolutions per day: | 15.08823014 |
| mean anomaly at epoch: | 267.6057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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