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 61674U 26145.26709213 +.00000000 +00000-0 +85668-4 0 00002
2 61674 53.1607 95.1213 0001343 86.9949 273.1205 15.30188220 05
| Epoch (UTC): | 25 May 2026 06:24:36 |
| Eccentricity: | 0.0001343 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.1213° |
| argument of perigee: | 86.9949° |
| revolutions per day: | 15.30188220 |
| mean anomaly at epoch: | 273.1205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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