▸Orbital parameters

Orbit class	SSO
Inclination	97.3240°
Eccentricity	0.0004677
Period	92.8 min
Apogee	413 km
Perigee	407 km
Mean motion	15.52395211 rev/day
RAAN	259.2291°
Arg of perigee	38.2413°
Mean anomaly	321.9171°
B*	5.2431e-4
Rev at epoch	19,564

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 55012U 23001D 26188.16466730 .00031987 00000-0 52431-3 0 9993

2 55012 97.3240 259.2291 0004677 38.2413 321.9171 15.52395211195648

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CONNECTA T1.2",
  "OBJECT_ID": "2023-001D",
  "EPOCH": "2026-07-07T03:57:07.255+00:00",
  "MEAN_MOTION": 15.52395211,
  "ECCENTRICITY": 0.0004677,
  "INCLINATION": 97.324,
  "RA_OF_ASC_NODE": 259.2291,
  "ARG_OF_PERICENTER": 38.2413,
  "MEAN_ANOMALY": 321.9171,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 55012,
  "REV_AT_EPOCH": 19564,
  "BSTAR": 0.00052431,
  "MEAN_MOTION_DOT": 0.00031987,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	CONNECTA T1.2
Operator	Plan-S Satellite and Space TechnologiesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Türkiye
Launch date	Jan 3, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/55012

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.