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 65898U 26073.05343420 +.00000000 +00000-0 +97770-3 0 00001
2 65898 53.1593 350.9865 0001092 105.7859 254.3262 15.30200178 08
| Epoch (UTC): | 14 March 2026 01:16:56 |
| Eccentricity: | 0.0001092 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 350.9865° |
| argument of perigee: | 105.7859° |
| revolutions per day: | 15.30200178 |
| mean anomaly at epoch: | 254.3262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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