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 53661U 26145.23919859 +.00000000 +00000-0 -47347-4 0 00008
2 53661 97.4484 25.1562 0001958 78.4390 281.7057 15.05651206 05
| Epoch (UTC): | 25 May 2026 05:44:26 |
| Eccentricity: | 0.0001958 |
| inclination: | 97.4484° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.1562° |
| argument of perigee: | 78.4390° |
| revolutions per day: | 15.05651206 |
| mean anomaly at epoch: | 281.7057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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