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 61549U 26145.34908440 +.00000000 +00000-0 +14398-4 0 00007
2 61549 53.1618 17.8858 0001109 91.7011 268.4117 15.30192189 06
| Epoch (UTC): | 25 May 2026 08:22:40 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.1618° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 17.8858° |
| argument of perigee: | 91.7011° |
| revolutions per day: | 15.30192189 |
| mean anomaly at epoch: | 268.4117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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