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 data is extracted from the following two-line orbital elements,
1 21610U 91050F 25197.74524528 .00000196 00000-0 71711-4 0 9993
2 21610 98.2377 253.3650 0004378 77.2152 282.9528 14.42655022784970
| Epoch (UTC): | 16 July 2025 17:53:09 |
| Eccentricity: | 0.0004378 |
| inclination: | 98.2377° |
| perigee height: | 746 km |
| apogee height: | 753 km |
| right ascension of ascending node: | 253.3650° |
| argument of perigee: | 77.2152° |
| revolutions per day: | 14.42655022 |
| mean anomaly at epoch: | 282.9528° |
| orbit number at epoch: | 78497 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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