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 65253U 26145.57168249 +.00000000 +00000-0 +15541-3 0 00003
2 65253 97.4496 188.3212 0002494 127.5035 232.6419 15.05655192 05
| Epoch (UTC): | 25 May 2026 13:43:13 |
| Eccentricity: | 0.0002494 |
| inclination: | 97.4496° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.3212° |
| argument of perigee: | 127.5035° |
| revolutions per day: | 15.05655192 |
| mean anomaly at epoch: | 232.6419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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