MDQUBESAT-2 is a payload in SSO orbit, operated by Innova Space, launched 2023.
Orbital data last updated 46 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | SSO |
| Inclination | 97.5306° |
| Eccentricity | 0.0009493 |
| Period | 90.6 min |
| Apogee | 309 km |
| Perigee | 296 km |
| Mean motion | 15.89869207 rev/day |
| RAAN | 235.1144° |
| Arg of perigee | 260.3143° |
| Mean anomaly | 99.7057° |
| B* | 1.5784e-3 |
| Rev at epoch | 13,382 |
This object is recorded as DECAYED (re-entered). These are the last known elements before re-entry — not a current orbit.
1 58665U 23185P 26142.11232597 .00467036 84283-4 15784-2 0 99962 58665 97.5306 235.1144 0009493 260.3143 99.7057 15.89869207133825{
"OBJECT_NAME": "MDQUBESAT-2",
"OBJECT_ID": "2023-185P",
"EPOCH": "2026-05-22T02:41:44.964+00:00",
"MEAN_MOTION": 15.89869207,
"ECCENTRICITY": 0.0009493,
"INCLINATION": 97.5306,
"RA_OF_ASC_NODE": 235.1144,
"ARG_OF_PERICENTER": 260.3143,
"MEAN_ANOMALY": 99.7057,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 58665,
"REV_AT_EPOCH": 13382,
"BSTAR": 0.0015784,
"MEAN_MOTION_DOT": 0.00467036,
"MEAN_MOTION_DDOT": 0.000084283
}Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.
| Name | MDQUBESAT-2 |
| Operator | |
| Country | Argentina |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |
| Decay date |