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 53050U 26145.49946022 +.00000000 +00000-0 -10637-4 0 00002
2 53050 97.4462 326.5125 0001635 74.4085 285.7322 15.05649205 00
| Epoch (UTC): | 25 May 2026 11:59:13 |
| Eccentricity: | 0.0001635 |
| inclination: | 97.4462° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 326.5125° |
| argument of perigee: | 74.4085° |
| revolutions per day: | 15.05649205 |
| mean anomaly at epoch: | 285.7322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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