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 61673U 26145.26920419 +.00000000 +00000-0 +14875-4 0 00006
2 61673 53.1603 95.1351 0001124 77.0019 283.1107 15.30204711 05
| Epoch (UTC): | 25 May 2026 06:27:39 |
| Eccentricity: | 0.0001124 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.1351° |
| argument of perigee: | 77.0019° |
| revolutions per day: | 15.30204711 |
| mean anomaly at epoch: | 283.1107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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