▸Orbital parameters

Orbit class	SSO
Inclination	97.4699°
Eccentricity	0.0000828
Period	94.7 min
Apogee	505 km
Perigee	504 km
Mean motion	15.20527419 rev/day
RAAN	302.6826°
Arg of perigee	123.4501°
Mean anomaly	236.6813°
B*	1.1178e-4
Rev at epoch	5,784

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 64555U 25135AD 26187.83708361 .00002375 00000-0 11178-3 0 9999

2 64555 97.4699 302.6826 0000828 123.4501 236.6813 15.20527419 57841

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CONNECTA IOT-10",
  "OBJECT_ID": "2025-135AD",
  "EPOCH": "2026-07-06T20:05:24.024+00:00",
  "MEAN_MOTION": 15.20527419,
  "ECCENTRICITY": 0.0000828,
  "INCLINATION": 97.4699,
  "RA_OF_ASC_NODE": 302.6826,
  "ARG_OF_PERICENTER": 123.4501,
  "MEAN_ANOMALY": 236.6813,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64555,
  "REV_AT_EPOCH": 5784,
  "BSTAR": 0.00011178,
  "MEAN_MOTION_DOT": 0.00002375,
  "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 IOT-10
Operator	Plan-S Satellite and Space TechnologiesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Türkiye
Launch date	Jun 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia 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/64555

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