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 65074U 26145.15038690 +.00000000 +00000-0 -97706-3 0 00008
2 65074 97.4521 222.1989 0001846 215.6641 144.4463 15.05620259 00
| Epoch (UTC): | 25 May 2026 03:36:33 |
| Eccentricity: | 0.0001846 |
| inclination: | 97.4521° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.1989° |
| argument of perigee: | 215.6641° |
| revolutions per day: | 15.05620259 |
| mean anomaly at epoch: | 144.4463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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