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 61216U 26145.21620014 +.00000000 +00000-0 +13227-4 0 00002
2 61216 53.1603 327.0881 0001523 90.7173 269.4003 15.30190605 07
| Epoch (UTC): | 25 May 2026 05:11:19 |
| Eccentricity: | 0.0001523 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 327.0881° |
| argument of perigee: | 90.7173° |
| revolutions per day: | 15.30190605 |
| mean anomaly at epoch: | 269.4003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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