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 65284U 26145.59855580 +.00000000 +00000-0 +19637-3 0 00000
2 65284 97.4458 198.0977 0002425 116.4617 243.6860 15.05657223 09
| Epoch (UTC): | 25 May 2026 14:21:55 |
| Eccentricity: | 0.0002425 |
| inclination: | 97.4458° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 198.0977° |
| argument of perigee: | 116.4617° |
| revolutions per day: | 15.05657223 |
| mean anomaly at epoch: | 243.6860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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