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 65321U 26145.64860147 +.00000000 +00000-0 +18899-3 0 00002
2 65321 97.7369 220.4662 0001557 291.3473 68.7579 14.91410944 08
| Epoch (UTC): | 25 May 2026 15:33:59 |
| Eccentricity: | 0.0001557 |
| inclination: | 97.7369° |
| perigee height: | 592 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 220.4662° |
| argument of perigee: | 291.3473° |
| revolutions per day: | 14.91410944 |
| mean anomaly at epoch: | 68.7579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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