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 65073U 26145.63497519 +.00000000 +00000-0 +45393-3 0 00003
2 65073 97.4505 222.7718 0001684 207.2740 152.8399 15.05662147 07
| Epoch (UTC): | 25 May 2026 15:14:21 |
| Eccentricity: | 0.0001684 |
| inclination: | 97.4505° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.7718° |
| argument of perigee: | 207.2740° |
| revolutions per day: | 15.05662147 |
| mean anomaly at epoch: | 152.8399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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